Process for forming one or more substantially pure layers in substrate material using ion implantation

ABSTRACT

A process is disclosed for forming a substantially pure monocrystalline layer of an implantable element in a monocrystalline substrate material by (a) selecting an implantable element and a monocrystalline substrate material to be implanted which, at the temperatures to be used, have limited mutual solubility in one another and do not form any intermediate phases with one another; (b) implanting a sufficient amount of the implantable element in the substrate material to permit formation of the desired substantially pure layer of the implantable element in the substrate material; and (c) annealing the implanted substrate material to form the desired layer. The annealing step may not be required if the desired layer was formed during the implantation. 
     Also disclosed is an article made by the process.

The invention described herein arose in the course of, or under, Contract No. W-7405-ENG-48 between the United States Department of Energy and the University of California.

This application is a Continuation In Part of application Ser. No. 07/391,904, filed Aug. 10, 1989 now U.S. Pat. No. 4,976,987 issued Dec. 11, 1990.

BACKGROUND OF THE INVENTION

This invention relates to a process for forming one or more substantially pure layers of an element in a material. More particularly, this invention relates to the formation of one or more substantially pure layers of an element in another element, compound, or solid solution by ion implantation.

Implantation of small amounts of ions of a particular element into a substrate such as crystalline silicon is well known in the construction of integrated circuit structures. For example, elements such as boron, phosphorus, or arsenic are implanted into a silicon substrate in small amounts to alter the electrical properties of the silicon. It is known to implant oxygen atoms into a silicon substrate in large concentrations to form silicon oxide layers by the combination or reaction of the implanted oxygen ions with the silicon in the substrate.

For example, Baerg et al. U.S. Pat. No. 4,700,454, teaches the implantation of a silicon substrate with oxygen ions to form an insulating layer and states that other ions which will react with silicon to form an insulating layer may be used instead of oxygen, such as nitrogen, to form a silicon nitride-like layer. Short et al., U.S. Pat. No. 4,749,660, teaches implanting sufficient oxygen ions into a silicon substrate to form a maximum concentration of two oxygen atoms per silicon atom to form a buried SiO₂ layer in the silicon substrate. Griffith, U.S. Pat. No. 4,786,608, also teaching the formation of a silicon oxide buried layer in a silicon substrate by oxygen ion implantation.

Implantations of other elements into an elemental substrate without reaction of the substrate atoms and the implanted ions to form a compound such as the above-described silicon oxide compound are also known. For example, Myers and Smugeresky, in an article entitled "Phase Equilibria and Diffusion in the Be-Al-Fe System Using High Energy Ion Beams", published in Metallurgical Transactions, Vol. 7A, at pp. 795-802 in 1976, describe the implantation of single crystal beryllium with 30-50 keV aluminum in dosages of 2-6×10¹⁶ aluminum atoms/cm² (i.e., peak aluminum concentrations <10 atomic %) followed by annealing at temperatures of 600° C. and 800° C. The authors reported observation of aluminum precipitates using transmission electron microscopy (TEM) after annealing.

Buene et al., in an article entitled "Metastable Alloys of Beryllium Prepared by Ion Implantation", published in Metallurgical Transactions, Vol. 15A, at pp. 1787-1804 in 1984, reported the implantation of beryllium with zinc at an energy of 185 keV with a 1.6×10¹⁷ zinc atoms/cm². Annealing at 600° C. for 10 minutes resulted in an increase in the peak zinc concentration of from 12 to about 17 atomic %.

However, others have not reported the formation of a substantially pure layer of an implanted element formed in another element, compound, or solid solution as a result of ion implantation. This is not surprising since sputtering of both the implanted substrate as well as atoms of the implanted element during implantation would appear to limit the maximum concentration of the implanted element in the substrate obtainable using ion implantation. Furthermore, diffusion of the implanted element away from the highest concentration regions during both the implant and the subsequent annealing step would also appear to limit the maximum concentration of the implanted element in the substrate obtainable by implantation. Finally, precipitation of intermediate phases containing elements of the substrate and the implanted element would be expected to interfere with the formation of the elemental layer.

SUMMARY OF THE INVENTION

It is, therefore, an object of this invention to provide a method for forming a substantially pure layer of an element into a substrate material which comprises another element, compound, or solid solution using ion implantation.

In accordance with the invention, the method comprises: (a) selecting an implantable element and a substrate material to be implanted which, at the temperatures to be used for the implantation and any subsequent anneal, (i) have limited mutual solubility in one another; and (ii) have an absence of intermediate phases formable between the implantable element and the material comprising the implanted substrate; and (b) implanting a sufficient amount of the implantable element to form the desired substantially pure layer of the implanted element in the substrate material either during implantation or during a subsequent anneal. In a preferred embodiment, an annealing step follows the implantation step.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a flow sheet illustrating the process of the invention.

FIG. 2 is a fragmentary cross-sectional view of a substrate having a substantially pure layer of an implanted element formed therein.

FIG. 3 is a bright field cross sectional electron microscopy (XTEM) photograph showing a buried monocrystalline aluminum layer and associated precipitate bands that formed in (1010) beryllium implanted with 11×10¹⁷ Al/cm² and subsequently annealed at 500° C. for 1h.

FIG. 4 is a comparison of Rutherford backscattering (RBS) spectra of the sample in FIG. 3 in the as-implanted (11×10¹⁷ Al/cm²) and annealed (500° C., 1h) states which shows that layer formation occurred during the post-implant anneal.

FIG. 5 is a plan view scanning electron microscopy (SEM) photograph (15 keV) revealing rectangular beryllium defects in the aluminum layer of the sample in FIG. 3 (11×10¹⁷ Al/cm² +500° C. for 1h).

FIG. 6 is a plot of peak aluminum concentration measured with RBS as a function of aluminum dose which indicates a critical dose dependence for layer formation in monocrystalline and polycrystalline beryllium.

DETAILED DESCRIPTION OF THE INVENTION

The invention comprises a process for forming a substantially pure layer of an element in a substrate which may comprise another element, a compound, or a solid solution of one or more elements in one or more elements.

By use of the term "substantially pure" with respect to the implanted layer is meant a layer of an implantable element having a purity determined by the solubility of the substrate material in the implanted element, but being at least 90 atomic percent (at. %).

By use of the term "layer" is meant that there is a region throughout that area of the substrate being implanted, containing mainly the implanted element, centered at some depth with a finite width such that the substrate and this region containing the implanted element are separated by an interphase boundary.

While the process of the invention may be used in connection with a number of materials, an important part of the process is the screening of materials for certain properties which must be exhibited prior to successful use of the materials in the process.

First of all, the element to be implanted in the substrate, sometimes herein referred to as either the "implantable element" or the "implanted element", and the substrate must have a limited solubility in one another at the temperatures used for implantation and for annealing of the implanted substrate. Thus, for example, the implantation of copper into nickel would form a copper/nickel solid solution because of the large mutual solubility of copper and nickel in one another. Such materials could not, therefore, be used together in the practice of this invention.

By "limited mutual solubility" is meant that the solubility of the implantable element in the substrate material is less than 10 at. %, preferably less than 5 at. %, and the solubility of the substrate material in the implantable element is less than 10 at. %, preferably less than 5 at. %.

Second, there must exist a finite temperature range in part of the phase diagram showing only the pure implantable element on one side and only the pure substrate material on the other side, without any intermediate phases in that temperature range. Thus, for example, the implantation of oxygen or nitrogen ions into a silicon substrate would be excluded from this process since both oxygen and nitrogen are reactive with silicon to form an intermediate phase consisting of silicon oxide (SiO₂) or silicon nitride (Si₃ N₄) when the respective ions are implanted into silicon at an implantation temperature of 350° C.

Examples of implantable elements and suitable substrate materials are shown in Table I, which is intended to be representative only. It also should be noted that the elements listed as suitable substrate materials may be interchanged with any one of the implantable elements listed for that substrate. For example, where Be, Al, Zn, Ag, Cd, Sn, Au, and Pb are listed in Table I as implantable elements in a silicon substrate, silicon may, instead be the implantable element in a substrate consisting of any one of those listed elements.

                  TABLE I                                                          ______________________________________                                         Substrate    Implantable Element                                               ______________________________________                                         1.    Be         Li, Al, Si, Zn, Ge, Ag, Sn                                    2.    C          Cu, Zn, As, Ag, Cd, Sn, Au                                    3.    Al         Na, K, Si, Zn, Ge, As, Cd, Pb                                 4.    Si         Be, Al, Zn, Ag, Cd, Sn, Au, Pb                                5.    Ti         Li, Mg, Y, La, Ce, Pu                                         6.    Fe         Li, Na, Mg, Ca, Cu, Ag, Cd, Sn, Pb                            7.    Ni         Li, Na, K, Ag, Pb                                             8.    Cu         Li, C, Na, Cr, Fe, Mo, Ag, W, Pb                              9.    Ge         Be, Al, Zn, Ag, Cd, Au, Pb                                    10.   U          Li, Na, Mg, Ca, Cr, Ag, W, Ce                                 ______________________________________                                    

The suitability of other pairs of elements for use, respectively, as the implantable element and the substrate in the practice of this invention may be readily determined, for example, by consulting the "Atlas of Binary Alloys" by Staudhammer and Murr, published in 1973 by Marcel Dekker, Inc. of New York. When a pair of elements are listed as not forming one or more intermediate phases, the phase diagram for these two elements should be consulted for limited mutual solubility between the pair in a particular temperature range shown on the phase diagram.

It should be noted here that the substrate into which the implantable element will be implanted may be an element, a compound, or a solid solution. However, the criteria discussed above apply equally whether or not the substrate is a single element or comprises more than one element. Whether the substrate comprises a single element, a compound, or a solid solution, the portion of the substrate being implanted should consist of a single-phase solid material. That is, the entire area of the substrate being implanted, over a depth range that will contain all of the implanted element, must be a homogeneous solid. Furthermore, the substrate may be monocrystalline, polycrystalline, or amorphous.

The purity of the implantable element which will be ionized in the ion source portion of the implantation apparatus will normally be at least 90 at. % and preferably at least about 95 at. %. It is recognized that in commercially available ion implantation apparatus in use today, the purity of the ion beam of the implantable element may be much higher due to the magnetic separation means through which the ion beam passes.

The purity of the element, compound, or solid solution comprising the substrate which is to be implanted by the implantable element should also have a purity of at least about 90 at. % and preferably at least about 95 at. %.

The temperature used for the implantation will normally range from about 77° K. (-196° C.) to about 10° C. below the melting point of the substrate. When a subsequent annealing step is carried out, the annealing temperatures will normally range from about 20° C. up to about 10° C. below the melting point of the substrate for a period of from about 1 second to about 100 hours, typically from about 0.2 to 2 hours.

It should be noted here that normally an annealing step will be carried out after the implantation step. However, in some instance where the implantation temperature is appropriately chosen, i.e., within the implantation temperature range, the annealing step may not be necessary.

It is, therefore, within these temperature ranges that one must screen the implantable element and the materials in the substrate to be implanted to determine whether or not, within these temperature ranges, these materials meet the above recited criteria of limited mutual solubility and lack of intermediate phases containing both the implantable element and the substrate material.

An additional criterion for the formation of the substantially pure layer of the implanted element is the extent of the implantation. This will include the energy of the implantable element, which will affect the depth of the implanted layer; and, most importantly, the amount or dosage of the implantable element which determines the concentration of the implanted element.

The energy of the implantable element may be varied to control the depth of the implantation, as stated above. The depth of the implanted element will also vary with the atomic mass of the implantable element. Normally, however, the energy of the implantable element will range from at least about 5 keV to about 2000 keV. As an example, the energy for the implantation of aluminum into beryllium ranges from about 5 keV (which will result in an implantation depth of about 11 nanometers (nm)) to about 2000 keV (which will result in an implantation depth of about 1900 nm).

It should be noted here that it is within the scope of the invention to provide a shallow implant to form a substantially pure layer of the implanted element which will extend to the surface of the substrate. When such a shallow implant is desired, the energy of the ions of the implantable element will be kept on the low end of the energy range.

It should also be noted that it is within the scope of the invention to form more than one substantially pure layer of the same implantable element, i.e., two or more layers, in a single substrate. Such may be accomplished, for example, by carrying out a first implant at a higher energy, to form a first deeper layer, followed by a shallower implant at a lower energy. It is also possible to use multiple implants of the same element at different energies to form a thicker layer of the implanted element than would be achieved by a single energy implantation. It is also within the scope of the invention to form two or more layers using different implantable elements for each layer, e.g., using a first implantable element to form the deeper layer and a second implantable element to form a second, shallower layer.

Even it all other criteria are met, failure to provide a certain minimum dosage of the implanted element will result in a failure to produce the substantially pure layer of implanted element of the invention. The minimum dosage, or fluence of the implantable element which must be implanted into the substrate to achieve the substantially pure layer of implanted element in accordance with the invention will be at least about 5×10¹⁶ atoms/cm², preferably at least about 5×10¹⁷ atoms/cm², and most preferably at least about 1.1×10¹⁸. This minimum dosage will, however, vary with the mass of the implanted element, its energy, and the particular substrate material. Thus, for example, in the prior art implantation of aluminum into beryllium by Myers and Smugeresky and the implantation of zinc into beryllium by Buene et al., as discussed above, the failure to provide a sufficient minimum dosage probably explains the failure to produce the substantially pure layers of the implanted element of this invention.

In a preferred embodiment the implantation, in accordance with the invention, will take place under conditions wherein sputtering, particularly sputtering of the substrate, will be inhibited or at least reduced to a level where the sputtering does not limit the implantation of sufficient atoms of the implantable element to form the substantially pure layer.

This may be accomplished by carrying out the implantation in the presence of a gas which will reduce the amount of sputtering, by the ion beam, of material from the surface of the substrate which is being implanted. Such gases react with the substrate material to form surface compounds that are sputtered more slowly than the substrate material.

Examples of gases which may be used to reduce the sputtering of either materials from the substrate being implanted or the implantable element include oxygen, water vapor, carbon dioxide, and nitrogen. The partial pressure of these gases in the implantation apparatus will range from about 10⁻⁷ to about 10⁻⁴ Torr.

Sputtering of the substrate during the implantation process may also be reduced by coating the substrate with a material having a lower sputtering rate than the substrate which will reduce such sputtering. Examples of such coating materials include beryllium, carbon and compounds such as beryllium oxide, silicon oxide, or aluminum oxide.

It should be noted that such coatings formed on the substrate to reduce sputtering, either by exposure to certain gases or by the use of coating materials applied to the substrate surface, do not need to meet the critieria for the implantable element or the substrate since such materials may be considered to be sacrificial materials which are either removed during the implantation (by sputtering) or may be removed after the implantation step.

If desired, after completion of the implantation process and formation of the substantially pure implanted layer in the substrate, a sufficient amount of the surface of the substrate, i.e., the surface layer, may also be removed by, for example, dry or wet etching means to expose the newly formed substantially pure implanted layer of the implantable element therein. Alternatively, as discussed above, the implanted substantially pure layer may be formed by a sufficiently shallow implant so as to extend the implanted layer to the surface of the substrate, thus making it unnecessary to remove any of the substrate material to expose the substantially pure implanted layer.

It should also be noted that if desired, a substantially pure patterned buried layer may be implanted by using an appropriate mask over the substrate or by using a focused ion beam or any other patterning means.

To further illustrate the process of the invention, a polycrystalline beryllium substrate was implanted with aluminum ions. For temperature below 570° C., the solubility of aluminum is less than 0.007 atomic percent and the solubility of beryllium in aluminum is less than 0.1 atomic percent. The beryllium substrate had a purity of greater than 99 at. % and a thickness of about 2 mm. The aluminum ions were implanted into the beryllium substrate at an energy of 200 keV to a fluence of 1.1×10¹⁸ aluminum atoms/cm² while maintaining the beryllium substrate at about 100° C. and in the presence of about 10⁻⁶ Torr of water vapor which tended to suppress sputtering. The aluminum-implanted beryllium substrate was then vacuum annealed at about 10.sup.×6 Torr at a temperature of about 570° C. for a period of about 1 hour. Cross-sectional transmission electron microscopy (XTEM) showed that an approximately 170 nm thick layer of substantially pure (>98 atomic %) aluminum had formed about 420 nm below the surface of the beryllium substrate, as shown in FIG. 2.

While the method of this invention is applicable to those situations in which the substrate is either a monocrystalline, polycrystalline or amorphous material, particularly advantageous results are obtained when the substrate is monocrystalline. In that event a monocrystalline layer of the implanted element is formed in the monocrystalline substrate. This particular embodiment of the invention is illustrated as follows.

Cylindrical samples (2 mm thick and 11.5 mm in diameter) of monocrystalline Be were spark cut with the circular faces within 2° of (1010) planes. The damage introduced by spark cutting was removed from the face to be implanted by first sanding with 600-grit paper and then electropolishing to remove an additional 100 μm. The samples were clamped to a water-cooled stage and implanted at 200 keV with a flux of 4.2 (±0.4)×10¹³ Al/cm^(2/) sec (as electronically rastered). Accurate temperature measurement during implantation was achieved by inserting a thermocouple junction into a spark cut hole in the side of each sample. During implantation the sample temperatures rose to between 38 and 65° C. Selected implanted samples were vacuum annealed at 500° C. for 1h in the low 10⁻⁷ Torr range.

FIG. 3 is a bright field XTEM micrograph showing the buried monocrystalline Al layer which formed during post-implant annealing of a sample implanted with 11×10¹⁷ Al/cm². The aluminum is in a diffracting condition and appears dark. The thickness of the layer varies between 120 and 150 nm, and the depth to the center of the layer varies between 380 and 410 nm. The orientation relationship between the Al layer and the Be matrix is shown. On either side of the layer are fairly equiaxed Al precipitates that generally decrease in size with distance from the layer. Immediately adjacent to the layer are precipitate-free zones--the zone on the deep side of the layer is noticeably wider than that on the shallow side. Very similar features were previously observed with XTEM in individual grains of polycrsytalline material implanted with 11.4×10¹⁷ Al/cm² and annealed at 570° C. for 1h [D.W. Brown et al., Appl. Phys. Lett. 54, 325 (1989)].

In FIG. 4 are RBS spectra comparing the as-implanted and annealed states of the sample shown in FIG. 3. The post-implant anneal produced a change from a Gaussian-like Al distribution to that of an 100 at. % Al layer with two associated side peaks corresponding to the precipitate bands.

The purity of the layer was further analyzed using Auger electron spectroscopy (AES) sputter profiling. The composition of the layer was found to be 97 at. % Al.

The lateral uniformity of the layer in FIG. 3 was examined using SEM. At sufficiently high incident electron energies (10 keV) the Al layer could be imaged through the Be overlayer. The micrograph in FIG. 5 was taken at normal incidence to the implanted surface to reveal a plan view of the layer. The dark, rectangular features are due to defects in the Al layer in the form of Be columns extending through the layer from the Be overlayer to the Be bulk. Several of the sparsely spaced defects were visible in a XTEM sample.

In FIG. 6 the peak Al concentration is plotted as a function of dose for both as-implanted and subsequently annealed samples. The two curves guide the eye through the data points for monocrystalline Be. For doses 9×10¹⁷ Al/cm², layer formation occurred during post-implant annealing. The RBS spectra for these annealed samples closely resembled the one in FIG. 4 except the peak concentration did not reach 100 at. % for doses 11×10¹⁷ Al/cm². For doses 8×10¹⁷ Al/cm², little change occurred in the peak concentration during annealing. Between 8 and 9×10¹⁷ Al/cm² a critical dependence on dose was found--an increase in the as-implanted peak concentration of only 12% caused the annealed peak concentration to increase by about 165%.

SEM of the annealed monocrystalline samples revealed that the critical dose dependence of layer formation corresponded to a critical dose dependence of the defect density in the resulting layer. For 13×10¹⁷ Al/cm² the defects were almost nonexistent and, on average, appeared slightly smaller than in FIG. 5. Between 13 and 9×10¹⁷ Al/cm² the density and size (and, thus, the areal fraction) of defects increased as the dose decreased. In the critical dose interval between 9 and 8×10¹⁷ Al/cm², a dramatic increase in the defect density occurred resulting in the abrupt drop in the Al concentration (FIG. 6).

From the foregoing, it is clear that a buried monocrystalline aluminum layer was formed in monocrystalline beryllium by implantation and post-implant annealing. The Al-Be system is only one of hundreds of binary systems that satisfy the equilibrium criteria of low mutual solubility and no intermediate phases.

Thus, the invention provides a process for forming a substantially pure layer of an implantable element in a substrate when the implantable element is implanted to a certain minimum concentration and the implantable element and the materials in the implanted substrate have low mutual solubility in one another and do not form intermediate phases with one another.

While specific embodiments of the process for implanting a substantially pure layer of an element into a substrate has been illustrated and described for carrying out the process in accordance with this invention, modifications and changes of the apparatus, parameters, materials, etc. will become apparent to those skilled in the art, and it is intended to cover in the appended claims all such modifications and changes which come within the scope of the invention. 

We claim:
 1. A process for forming a substantially pure, monocrystalline layer of an implantable element in a monocrystalline substrate which comprises:(a) selecting an implantable element and a monocrystalline substrate material to be implanted which, at the temperature to be used for the implantation:(i) have limited mutual solubility in one another; and (ii) do not form intermediate phases with one another; and (b) implanting a sufficient amount of the implantable element to form said desired substantially pure, monocrystalline layer of the implantable element in the monocrystalline substrate material.
 2. The process of claim 1 wherein said implanted substrate is annealed at a temperature not exceeding about 10° C. below the melting point of the substrate to form said substantially pure layer.
 3. The process of claim 2 wherein said implanted substrate is annealed at a temperature which ranges from at least about 20° C. up to about 10° C. below the melting point of the substrate to form said substantially pure layer.
 4. The process of claim 1 wherein at least 5×10¹⁶ atoms/cm² of said implantable element are implanted in said substrate material to form said substantially pure layer therein.
 5. The process of claim 1 wherein at least about 5×10¹⁷ atoms/cm² of said implantable element are implanted in said substrate material to form said substantially pure layer therein.
 6. The process of claim 1 wherein the solubility of said implantable element in said substrate material is less than about 10 at. %.
 7. The process of claim 1 wherein the solubility of said implantable element is said substrate material is less than about 5 at. %.
 8. The process of claim 1 wherein the solubility of said substrate material in said implantable element is less than about 10 at. %.
 9. The process of claim 1 wherein the solubility of said substrate material in said implantable element is less than about 5 at. %.
 10. The process of claim 1 wherein said implantation step is carried out at a temperature ranging from about -196° C. to about 10° C. below the melting point of the substrate.
 11. The process of claim 1 wherein said implantation step is carried out at a temperature within the implantation temperature range to permit formation of said substantially pure layer of said implantable element without a post-implant annealing step.
 12. The process of claim 1 wherein said implantable element is implanted into said substrate at an energy ranging from about 5 keV to about 2000 keV.
 13. The process of claim 1 wherein said implantation is carried out in the presence of a gas capable of reducing sputtering of said substrate materials during the implantation process.
 14. The process of claim 13 wherein said gas capable of inhibiting sputtering during said implantation process is selected from the class consisting of oxygen, water vapor, carbon dioxide, and nitrogen.
 15. The process of claim 1 including the further step of providing a coating on said substrate which will inhibit sputtering during said implantation process.
 16. The process of claim 1 including the further step of exposing said substantially pure implanted layer after said implantation step by removing the surface layer of said substrate to expose said implanted layer.
 17. The process of claim 16 wherein said step of removing a portion of said substrate to expose said implanted layer is carried out by sputtering, wet etching, dry etching, or by mechanical means.
 18. The process of claim 1 wherein said implantation step comprises forming a shallow implant of said implantable element to form said substantially pure implanted layer so as to be exposed adjacent to the surface of said substrate.
 19. The process of claim 1 wherein said implantation step is carried out two or more times at different energies to thereby form two or more of said substantially pure layers in said substrate.
 20. The process of claim 19 wherein said two or more implantation steps are carried out using the same implantable element to form two or more layers or one or more thicker layers of the same implanted element in said substrate.
 21. The process of claim 19 wherein said two or more implantation steps are carried out using different implantable elements to form two or more layers of different implanted elements in said substrate.
 22. The process of claim 1 wherein said step of forming said substantially pure layer in said substrate further includes forming a patterned buried layer in said substrate.
 23. The process of claim 22 wherein said patterned layer in said substrate is formed by the step of masking said substrate prior to said implantation step.
 24. The process of claim 22 wherein said patterned layer is formed in said substrate by using a focused ion beam to implant a pattern layer in said substrate.
 25. A process for forming a substantially pure layer of an implantable element in a monocrystalline substrate which comprises:(a) selecting an implantable element and a monocrystalline substrate to be implanted wherein, at the temperature to be used for the implantation:(i) the solubilities of said implantable element and said substrate material in one another are less than 10 at. %; and (ii) no intermediate phases containing both said implantable element and said substrate material exist; and (b) implanting, at a temperature ranging from about -196° C. to about 10° C. below the melting point of the substrate, at least about 5×10¹⁶ atoms/cm² of said implantable element in said substrate; to form said monocrystalline layer of said implantable element having a purity of at least about 90 at. % in said monocrystalline substrate.
 26. A process for forming a substantially pure, monocrystalline layer of an implantable element in a monocrystalline substrate which comprises:(a) selecting an implantable element and a monocrystalline substrate to be implanted wherein, at the temperature to be used for the implantation and annealing:(i) the solubilities of said implantable element and said substrate material in one another are less than 10 at. %; and (ii) no intermediate phases containing both said implantable element and said substrate material exist; (b) implanting, at a temperature ranging from about -196° C. to about 10° C. below the melting point of the substrate, at least about 5×10¹⁶ atoms/cm² of said implantable element in said substrate; and (c) annealing said implanted substrate at a temperature ranging from about 20° C. to about 10° C. below the melting point of the substrate for a period of about 1 second to about 100 hours;to form said monocrystalline layer of said implantable element having a purity of at least about 90 at. % in said monocrystalline substrate.
 27. A process for producing a substantially pure, monocrystalline layer of aluminum in a beryllium substrate which comprises:(a) implanting aluminum ions into a monocrystalline beryllium substrate at an energy of about 200 keV and fluence of at least about 1.1×10¹⁸ atoms/cm² while maintaining the temperature below about 150° C.; and (b) annealing said implanted beryllium substrate at a temperature of from about 400° C. to just below 570° C. for a period of from about 0.2 to 4 hours; to form said layer of substantially pure monocrystalline aluminum in said monocrystalline beryllium substrate.
 28. A method of making an article of manufacture consisting of a host material containing an essentially pure, implanted elemental species layer having compositionally abrupt interfaces between said host material and said layer, comprising the following steps:a) providing a single phase host material which is of limited mutual solubility with respect to the elemental species and has an absence of intermediate phases involving said implanted elemental species; b) implanting an elemental species into the material through the surface of said material such that a sufficient amount of said implanted species to form a distinct layer is entirely within the host material, said material being held at a predetermined temperature; and c) optionally heat treating, said implanted material in an environment such that a pure, buried, elemental layer is formed inside said host material.
 29. The method of claim 28, wherein said host material is a monocrystalline material and said implanted, buried layer is monocrystalline and has a preferred crystallographic orientation related to that of the host material.
 30. The method of claim 28, wherein said host material is sputtered during implantation, and the sputtering of said host material during implantation is reduced by a partial pressure of a gas that reacts with the material forming a thin, stable surface compound that has a low sputtering rate and, yet, allows for the implantation of the desired species inside the host material.
 31. The method of claim 28, wherein said host material is sputtered during implantation, and the sputtering of said host material during implantation is reduced by a thin, stable surface compound previously formed on the surface of the host material that has a low sputtering rate and, yet, allows for the implantation of the desired species inside the host material.
 32. The method of claim 28, wherein the host material between the implanted layer and the surface is removed by at least one of sputtering, chemical etching, electrochemical etching, and mechanical means to leave a pure, elemental, integral layer at an external surface of the host material.
 33. The method of claim 28, wherein the temperature of the host material during the implantation is maintained sufficiently high to lead directly to the formation of the pure, elemental layer without post-implant annealing.
 34. The method of claim 28, wherein masks, focused ion beams, or other means lead to the formation of a patterned, buried-layer structure.
 35. The method of claim 28, wherein multiple pure, buried layers are formed at various depths by implantation of one of (i) the same elemental species using various ion energies, (ii) different elemental species using the same ion energies, or (iii) different elemental species using various ion energies.
 36. A method of making an article of manufacture consisting of a host material containing an essentially pure, ion implanted elemental species layer having compositionally abrupt interfaces between said host material and said layer, comprising the following steps:a. providing a single phase host material which is of limited mutual solubility with respect to the elemental species and has an absence of intermediate phases involving said implanted elemental species; b. implanting an elemental species into the material at a depth sufficiently shallow, to provide formation of a pure, elemental, integral layer at an external surface of said host material, said material being held at a predetermined temperature; and c. optionally heat treating said implanted material. 